Classifications

• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
  • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
  • F17C3/00—Vessels not under pressure
  • F17C3/02—Vessels not under pressure with provision for thermal insulation
  • F17C3/025—Bulk storage in barges or on ships
  • F17C3/027—Wallpanels for so-called membrane tanks
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
  • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
  • B63B25/00—Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby
  • B63B25/02—Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby for bulk goods
  • B63B25/08—Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby for bulk goods fluid
  • B63B25/12—Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby for bulk goods fluid closed
  • B63B25/16—Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby for bulk goods fluid closed heat-insulated
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
  • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
  • B63B27/00—Arrangement of ship-based loading or unloading equipment for cargo or passengers
  • B63B27/24—Arrangement of ship-based loading or unloading equipment for cargo or passengers of pipe-lines
  • B63B27/25—Arrangement of ship-based loading or unloading equipment for cargo or passengers of pipe-lines for fluidised bulk material
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
  • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
  • B63B27/00—Arrangement of ship-based loading or unloading equipment for cargo or passengers
  • B63B27/30—Arrangement of ship-based loading or unloading equipment for transfer at sea between ships or between ships and off-shore structures
  • B63B27/34—Arrangement of ship-based loading or unloading equipment for transfer at sea between ships or between ships and off-shore structures using pipe-lines
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
  • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
  • B63B3/00—Hulls characterised by their structure or component parts
  • B63B3/14—Hull parts
  • B63B3/68—Panellings; Linings, e.g. for insulating purposes
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
  • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
  • F17C2201/00—Vessel construction, in particular geometry, arrangement or size
  • F17C2201/01—Shape
  • F17C2201/0147—Shape complex
  • F17C2201/0157—Polygonal
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
  • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
  • F17C2201/00—Vessel construction, in particular geometry, arrangement or size
  • F17C2201/05—Size
  • F17C2201/052—Size large (>1000 m3)
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
  • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
  • F17C2203/00—Vessel construction, in particular walls or details thereof
  • F17C2203/03—Thermal insulations
  • F17C2203/0304—Thermal insulations by solid means
  • F17C2203/0358—Thermal insulations by solid means in form of panels
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
  • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
  • F17C2203/00—Vessel construction, in particular walls or details thereof
  • F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
  • F17C2203/0602—Wall structures; Special features thereof
  • F17C2203/0612—Wall structures
  • F17C2203/0626—Multiple walls
  • F17C2203/0631—Three or more walls
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
  • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
  • F17C2209/00—Vessel construction, in particular methods of manufacturing
  • F17C2209/23—Manufacturing of particular parts or at special locations
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
  • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
  • F17C2221/00—Handled fluid, in particular type of fluid
  • F17C2221/03—Mixtures
  • F17C2221/032—Hydrocarbons
  • F17C2221/033—Methane, e.g. natural gas, CNG, LNG, GNL, GNC, PLNG
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
  • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
  • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
  • F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
  • F17C2223/0146—Two-phase
  • F17C2223/0153—Liquefied gas, e.g. LPG, GPL
  • F17C2223/0161—Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
  • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
  • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
  • F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
  • F17C2223/033—Small pressure, e.g. for liquefied gas
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
  • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
  • F17C2260/00—Purposes of gas storage and gas handling
  • F17C2260/01—Improving mechanical properties or manufacturing
  • F17C2260/011—Improving strength
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
  • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
  • F17C2270/00—Applications
  • F17C2270/01—Applications for fluid transport or storage
  • F17C2270/0102—Applications for fluid transport or storage on or in the water
  • F17C2270/0105—Ships
  • F17C2270/0107—Wall panels

Definitions

• the invention relates to the field of the manufacture of sealed and thermally insulated tanks.
• the present invention relates to tanks for containing cold liquids, for example tanks for the storage and / or transport of liquefied gas by sea.
• LNG liquefied natural gas
• LNG liquefied natural gas
• Such embedded tanks may be intended for example for the transport of LNG or to supply propulsion machinery for a ship.
• Such a tank is described in the document FR2691520.
• This tank is integrated into a supporting structure having longitudinally adjacent faces forming ridges.
• the vessel wall includes a sealing membrane which has a plurality of corrugated plates.
• the corrugations of the plates extend towards the inside of the tank so as to deform transversely to follow elastically any deformations of the tank wall elements supporting the sealing membrane or the thermal deformations of the membrane.
• the membrane has flexible corner pieces. These corner pieces comprise wave complementary wave sections provided on the corrugated plates of the membrane carried by the two walls of the tank forming the edge.
• An idea underlying the invention is to allow the realization of a corner piece of tank sealing membrane easy to manufacture and adapt to different tank shapes while effectively supporting the forces experienced by the membrane of sealing.
• the invention provides a sealed and thermally insulating tank intended to be integrated in a polyhedral bearing structure, the tank comprising a plurality of flat tank walls, each tank wall comprising at least one insulating barrier and at least one a waterproofing membrane, said insulating barrier consisting of a plurality of heat-insulating elements, each heat-insulating element comprising an insulating foam block, said insulating barrier carrying a plurality of sealing metal plates fixed to each other in a leak-tight manner; in order to form the sealing membrane, wherein a first and an adjacent second vessel wall form an edge, the vessel further comprising a sealing corner member located at the edge, the workpiece angle comprising:
• corner angle of sheet metal located along the edge, the corner angle having a first section which develops in the plane of the sealing membrane of the first vessel wall and a second section which develops in the plane of the sealing membrane of the second tank wall,
• each reinforcing wing respectively comprising a membrane section and an anchoring section;
• the insulating barrier of the first vessel wall has a first clearance formed in the insulating foam blocks along the edge
• the insulating barrier of the second vessel wall has a second clearance formed in the insulating foam blocks along the the ridge, the first clearance and the second clearance together forming a groove along the ridge
• the membrane section of the first reinforcing wing develops in the plane of the sealing membrane of the first tank wall between the first section of the corner angle and the insulating barrier of the first tank wall or the first locking piece, the first section of the corner angle being fixed to the membrane section of the first reinforcing wing,
• the membrane section of the second reinforcing wing develops in the plane of the sealing membrane of the second tank wall between the second section of the corner angle and the insulating barrier of the second tank wall or the second locking piece, the second section of the corner angle being fixed to the membrane section of the second reinforcing wing,
• the anchoring section of the first reinforcing wing, the anchoring section of the second reinforcing wing and the locking pieces are housed in the groove
• the first locking piece is fixed to the insulating barrier of the first tank wall in the first clearance and has an upper surface covered by the membrane section of the first reinforcing wing,
• the second locking piece is fixed to the insulating barrier of the second tank wall in the second clearance and has an upper surface covered by the membrane section of the second reinforcing wing,
• the anchoring section of the first reinforcing wing and the anchoring section of the second reinforcing wing each comprise a connecting section arranged, in the assembled state of the corner piece, between the two locking pieces and extend respectively from the membrane section of the first reinforcing wing, respectively second reinforcing wing, to a bottom of the groove,
• the anchoring section of the first reinforcing wing and the anchoring section of the second reinforcing wing each comprise a tab folded against a lower face of the first locking piece, respectively of the second locking piece, and arranged at the back of the throat,
• the lug of the first reinforcing wing is fixed on the lower face of the first locking piece and the lug of the second reinforcing wing is fixed on the lower face of the second locking piece.
• such a tank may comprise one or more of the following characteristics.
• the first clearance comprises on the one hand a lateral internal surface extending in the thickness direction of the tank wall and, on the other hand, a bottom,
• the second clearance comprises on the one hand a lateral internal surface extending in the thickness of the tank wall and, on the other hand, a bottom, the bottom of the first clearance and the bottom of the second clearance together forming a bottom of the throat,
• the first locking piece has a lateral external surface opposite to the second locking piece, the lateral external face of the first locking piece being fixed, for example by gluing, to the internal lateral face of the first release
• the second locking piece has a lateral external surface opposite to the first locking piece, the lateral external face of the second locking piece is fixed, for example by gluing, to the lateral internal face of the second clearance, the lower face of the first locking piece and the lug of the first reinforcing wing are fixed, for example by gluing, to the bottom of the first clearance,
• the lower face of the second locking piece and the lug of the second reinforcing wing are fixed, for example by gluing, to the bottom of the second clearance.
• the lower face of the first locking piece and the lower face of the second locking piece each comprise a countersink in which are lodged respectively the legs of the first reinforcing wing and the second reinforcing wing.
• a surface of the lower face of the first non-countersunk locking member is fixed on the bottom of the first clearance and a surface of the lower face of the second non-countersunk locking member is secured to the bottom of the second clearance.
• the first locking piece is connected to the second locking piece by a mechanical element engaged in the locking pieces perpendicularly to the edge.
• the mechanical element comprises a screw associated with a nut.
• each locking piece consists of an elongated beam extending along the edge, the beam of the first locking piece extending parallel to the beam of the second locking piece, a plurality of mechanical elements. connect the first locking piece and the second locking piece along the beam,
• the anchoring section of the reinforcing wings develops between the two locking pieces between two consecutive mechanical elements and is interrupted at the level of the mechanical elements.
• the insulating barrier of the first vessel wall and the insulating barrier of the second vessel wall each have an end surface extending parallel in the thickness direction of the vessel wall, the end surfaces of the insulating barrier of the first vessel wall and the second vessel wall being secured together.
• the end surface of the insulating barrier of the first vessel wall and the end surface of the insulating barrier of the second vessel wall are bonded together.
• the insulating barrier of the first vessel wall and the insulating barrier of the second vessel wall each have an end surface extending parallel in the thickness direction of the vessel wall, the surfaces end of the insulating barrier of the first vessel wall and the second vessel wall not being fixed together.
• the mechanical element linking the first locking piece and the second locking piece is elastically deformable in a direction perpendicular to the end surfaces of the insulating barrier of the first and second tank wall so as to the connection between the first locking piece and the second locking piece is elastic.
• the anchoring section of one of the reinforcing wings comprises, in a plane perpendicular to the edge, a stiffener connecting the junction section and the leg of the reinforcing wing, the locking piece. covered by the membrane section of said reinforcing wing having a groove in which the stiffener is housed.
• a plurality of stiffeners are located on each reinforcing wing regularly spaced along the fold between the tab and the joining section, each locking piece having a plurality of grooves in which are housed the plurality of stiffeners.
• the locking piece is made of high density foam.
• the locking piece is made of wood.
• the angle is a continuous metal plate.
• the angle and reinforcing wings of the corner piece are made of metal sheet with a low coefficient of expansion.
• the tab of the first reinforcing wing and the tab of the second reinforcing wing are fixed respectively against the first locking piece and the second locking piece by a screw.
• the insulating barrier of each wall comprises an insulating foam block and a wood panel, the wood panel covering an upper face of the insulating foam block.
• the sealing membrane of the first tank wall is sealingly attached to the first section of the corner angle and the sealing membrane of the second tank wall is sealingly secured to the second section of the corner angle.
• the corner angle develops along the axis of the edge towards the outside of the corner piece beyond the blocking pieces.
• the corner angle comprises a central wave directed towards the inside of the tank and developing perpendicularly to the edge.
• each wall of the tank comprises, from the inside of the tank to the outside of the tank:
• the primary and secondary insulation barriers each comprise insulating foam blocks juxtaposed, the foam blocks of the primary insulating barrier being bonded to the secondary waterproof membrane, the secondary waterproof membrane being bonded to the foam blocks of the insulating barrier secondary, the foam blocks of the primary insulating barrier of the first vessel wall having the first clearance disposed along the edge and the foam blocks of the primary insulating barrier of the second vessel wall having the second clearance disposed on the along the ridge.
• the first clearance and the second clearance are formed over the entire thickness of the insulating foam blocks of the primary insulating barrier respectively of the first tank wall and the second tank wall, so that the bottom groove is formed by the sealed composite film layer of the secondary sealing membrane respectively of the first vessel wall and the second vessel wall.
• the corner angle comprises a lower angle plate and an upper angle plate superimposed and fixed together, and wherein the membrane sections of the reinforcing wings are fixed on the corner plate lower and the first and second sections of the upper corner plate cooperate with the end plates of the primary sealing membrane respectively of the first vessel wall and the second vessel wall.
• the first blocking piece has a length in the plane of the first tank wall greater than the thickness of the primary insulating barrier and the second blocking piece has a length in the plane of the second wall of the tank. tank greater than the thickness of the primary insulating barrier.
• the vessel has an overall polygonal cylinder shape, the planar walls of the vessel including a polygonal bottom wall and a plurality of peripheral side walls each rising around the bottom wall from a respective side of the polygonal bottom wall, the vessel having a plurality of said corner pieces, each corner piece being arranged at the edge formed between one side of the bottom wall and the corresponding side wall.
• Such a tank can be part of a land storage facility, for example to store LNG or be installed in a floating structure, coastal or deep water, including a LNG tank, a floating storage and regasification unit (FSRU) , a floating production and remote storage unit (FPSO) and others.
• FSRU floating storage and regasification unit
• FPSO floating production and remote storage unit
• a vessel for the transport of a cold liquid product comprises a double hull and a aforementioned tank disposed in the double hull.
• the invention also provides a method of loading or unloading such a vessel, in which a cold liquid product is conveyed through isolated pipes from or to a floating or land storage facility to or from the vessel vessel.
• the invention also provides a transfer system for a cold liquid product, the system comprising the abovementioned vessel, insulated pipes arranged to connect the vessel installed in the hull of the vessel to a floating storage facility. or terrestrial and a pump for driving a flow of cold liquid product through the insulated pipelines from or to the floating or land storage facility to or from the vessel vessel.
• Some aspects of the invention start from the idea of providing a corner piece that supports the different cases of loading the waterproofing membrane. Another aspect of the invention is to allow the production of such a corner piece for a double-diaphragm seal tank, said corner piece can be used for both a primary membrane and a secondary membrane.
• One aspect of the invention starts from the idea of allowing a flexible connection between the insulation barriers of two adjacent vessel walls forming an edge.
• One aspect of the invention is to reduce the stresses of the corner piece due to thermal stresses.
• Another aspect of the invention is to allow a solid connection between the blocking parts and the insulating barrier. For this, one aspect of the invention starts from the idea of favoring the work in traction rather than in shear at the level of the fixing between the locking pieces and the insulating barriers.
• FIG. 1 is a sectional view along the axis II-II of FIG. 3 of an angle between two longitudinal walls of a sealed and thermally insulating storage tank comprising a corner piece anchored in the insulating barrier of FIG. tank ;
• Figure 2 is an exploded schematic perspective view of a corner piece of Figure 1;
• Figure 3 is a schematic perspective view of the corner piece of Figure 2 in the assembled state
• FIG. 4 represents a schematic perspective view of another embodiment of the corner piece in the mounted state.
• FIG. 5 is a sectional view of the bowl angle of FIG. 1 along axis IV-IV of FIG. 3, namely at the level of a mechanical element linking the first locking piece and the second piece of blocking blocking;
• Figure 6 is a sectional view of a vane angle having a double insulating barrier and a double sealing membrane and wherein a corner piece of Figures 2 and 3 is provided for each sealing membrane;
• Fig. 7 is a cutaway perspective view of the vial angle of Fig. 6 in which a corner piece according to a second embodiment is used;
• Figure 8 is a cutaway perspective view of the vial angle of Figure 6 in which the primary barrier was omitted at the angle to reveal the secondary barrier;
• Figure 9 is a schematic perspective cutaway view of an alternative embodiment of a vane angle of Figure 8 having a plurality of corner angles according to another embodiment
• FIG. 10 is a cutaway schematic representation of a sealed and thermally insulating tank integrated in a LNG tanker and of a loading / unloading terminal of this tank,
• FIG. 11 is a schematic perspective exploded view and a prefabricated corner element used in an angle between two perpendicular walls of a tank according to another embodiment in which an angle is omitted;
• Figure 12 is a partial schematic perspective view of an assembly of two prefabricated corner elements of Figure 11;
• FIG. 3 is a partial schematic perspective view of a prefabricated corner element of FIG. 11 in the mounted state in which a lower angle is fixed on the reinforcement wings;
• FIG. 14 is a diagrammatic perspective view in section of a vane angle employing prefabricated corner elements according to the embodiment of FIG. 11, on which an angle is arranged along the edge and the blocks. insulators adjacent the peripheral corner elements, and wherein the primary membrane is omitted;
• FIG. 15 is a partial perspective view of an angle between a polygonal bottom wall and side walls of a polygonal cylindrical vessel having prefabricated corner elements according to the embodiment of FIG. 11 and partially showing a primary membrane.
• Such a carrier structure has a prismatic structure. More precisely, longitudinal walls extend parallel to the longitudinal direction of the ship and form a polygonal section in a plane perpendicular to the longitudinal direction of the ship. The longitudinal walls are joined in longitudinal edges, which form for example angles of the order of 135 ° in an octagonal geometry.
• each wall of the carrier structure (not shown) carries a tank wall.
• Each of the tank walls is composed of at least one thermally insulating barrier 2 carrying a sealing membrane 3.
• a thermally insulating barrier 2 consists of a plurality of heat insulating elements (not shown). Each insulating element comprises a block of insulating foam on which is fixed a plywood panel. These heat-insulating elements are juxtaposed according to a regular rectangular mesh over the entire surface of the walls of the supporting structure to form a flat surface on which the sealing membrane 3 is anchored. Anchors (not shown) retain the heat-insulating elements. resting on the supporting structure. Such anchoring members are described in particular in the French patent application published under the number FR2691520. The anchoring members are attached to the support structure by means of studs (not shown) welded to the supporting structure. The heat-insulating elements of the thermally insulating barrier 2 rest on the carrier walls by means of cords of mastic forming parallel lines that are rectilinear or wavy.
• a sealing membrane 3 consists of a plurality of metal plates 5 juxtaposed to each other with overlap. These metal plates 5 are welded together to ensure the sealing of the sealing membrane 3.
• the metal plates 5 comprise a plurality of corrugations oriented towards the inside of the tank. These corrugations deform in response to stresses in order to maintain the tightness of the waterproofing membrane 3.
• Figure 1 shows a detail sectional view of a sealed and thermally insulating storage vessel angle at a longitudinal edge of the vessel having a corner piece anchored in the insulating barrier of the vessel.
• a heat-insulating element of angle 9,10 is disposed in the insulating barrier 2 on each side of a bisecting plane 11 formed by the two tank walls 6 and 7.
• An end face 12 of the angle insulating element 9 of the first vessel wall 6 is joined along the edge 8 with an end face 13 of the corner insulating element 10. of the second vessel wall 7.
• the corner elements 9, 10 are adjacent to each side of the bisecting plane 11.
• the corner elements 9, 10 each comprise an insulating foam block 14, 15.
• This block of Insulating foam 14, 15 is for example a block made of high density polyurethane foam, for example of the order of 130 Kg / m 3 .
• the heat-insulating elements of angles 9, 10 also comprise a plywood panel 16, 17. This plywood panel 16, 17 is located on an upper face 18, 19 of the insulating foam blocks respectively 14, 5.
• the elements of 9, 10 extend parallel to the walls of the carrier structure (not shown).
• the corner elements 9, 10 are independent of the other adjacent heat insulating elements (not shown) respectively of the first tank wall 6 and the second tank wall 7.
• Each heat insulating element 9, 10 has a cutout. This cut is made along the upper longitudinal edge 20, 21 of the heat insulating elements 9, 10 which is adjacent to the bisecting plane 11. These cuts of the heat-insulating elements 9, 10 delimit a half-groove respectively 22, 23 Each half-groove 22, 23 has a bottom 24, 25 extending in a plane perpendicular to the bisecting plane 1 1. Each half-groove 22, 23 has a lateral internal face 26, 27 extending in a plane parallel to the bisecting plane 11.
• each half-groove 22, 23 extends from the bottom of the half-grooves 24, 25 to an upper face 28, 29 of the heat-insulating elements 9, 10
• the cutouts forming the half-grooves 22, 23 are in the insulating foam blocks 14, 15 and in the wood panels plywood 16, 17.
• These two half-grooves 22, 23 are symmetrical with respect to the bisecting plane 11 and jointly form a groove 30.
• a bottom of the groove 31 is formed jointly by the bottom 24 of the first half-groove 22 and the bottom 25 of the second half-groove 23.
• an angle piece 32 is housed in the groove 30.
• a metal end plate 5 of the first tank wall 6 and a end plate 5 of the second tank wall 7 are both sealingly attached to the corner piece 32.
• Such a sealing connection is for example made by welding the metal end plates 5 of the walls 6.7 of the bowl 32 has a first locking piece 33 and a second locking piece 34.
• the corner piece 32 also comprises a first reinforcing wing 35 and a second reinforcing wing 36.
• the corner piece 32 also has a corner angle 37.
• the first locking piece 33 is of complementary shape to the first half-groove 22.
• the first locking piece 33 is made in the form of a wooden beam extending in the first half-groove 22 along the edge 8.
• the first blocking piece 33 has an upper face 38 extending in the plane of the upper face 28 of the heat-insulating element 9 of the first tank wall 6.
• the first blocking piece 33 has a lateral external face 39 extending along the lateral internal face 26 of the first half-groove 22.
• the first locking piece 33 has a lateral internal face 40 opposite to the lateral external face 39 and extending parallel to the bisecting plane 11.
• the first locking piece 33 has a lower face 41 extending along the bottom 24 of the first half-groove 22.
• the lateral external face 39 of the first locking piece 33 is intended to be fixed against the inter face. lateral side 26 of the first half-groove 22, for example by gluing.
• the lower face 41 of the first locking piece 33 is intended to be fixed against the bottom 24 of the first half-groove 22, for example by gluing.
• the second locking piece 34 is complementary in shape to the second half-groove 23 and is symmetrical to the first locking piece 33 with respect to the bisecting plane 11.
• the second locking piece 34 has an upper face 42, a face external lateral 43, a lateral internal face 44 and a lower face 45.
• the lateral external face 43 of the second piece of blocking 34 is intended to be fixed against the lateral internal face 27 of the second half-groove 23, for example by gluing.
• the lower face 45 of the second locking piece 34 is intended to be fixed against the bottom 25 of the second half-groove 23, for example by gluing.
• the first reinforcing wing 35 comprises a membrane section 46 and an anchoring section 47.
• the first reinforcing wing 35 is made in the form of a folded metal plate extending along the edge 8.
• the membrane section 46 of the first reinforcing wing 35 develops in the plane of the sealing membrane 3 of the first tank wall 6.
• the membrane section 46 of the first reinforcing wing 35 covers the upper face 38 of the the first locking piece 33.
• An end 48 of the membrane section 46 is joined to the anchoring section 47 of the first reinforcing wing 35.
• the first end 48 of the membrane section 46 is adjacent to the bisecting plane 11.
• the anchoring section 47 of the first reinforcing wing 35 has a junction section 49 and a tab 50.
• the junction section 49 develops parallel to the bisecting plane 11 along said bisecting plane 11.
• a first end 51 of the section junction 49 is joined to the end 48 of the membrane section 46.
• a second end 52 of the junction section 49 opposite its first end 51 is adjacent to the bottom 31 of the groove 30.
• the second end 52 is contiguous with the paw 50.
• the tab 50 of the anchoring section 47 of the first reinforcing wing 35 is folded against the lower face 41 of the first locking piece 31.
• the first reinforcing wing 35 is of complementary shape to the first locking piece 33.
• the first reinforcing wing 35 matches the upper face 38, the lateral internal face 40 and the lower face 41 of the first locking piece 33.
• the first reinforcing wing 35 is fixed to the first locking piece 33 by any means adapted, for example by screwing the tab 50 of the first reinforcing wing 35 on the lower face 41 of the first locking piece 22. Such screwing is for example achieved using wood screws 53.
• the second reinforcing wing 36 is similar to the first reinforcing wing 35.
• This second reinforcing wing comprises a membrane section 54 and a section Anchoring section 55 of the second reinforcing wing 36 has a connecting section 56 and a tab 57.
• the second reinforcing wing 36 is symmetrical to the first reinforcing wing 35 with respect to the bisecting plane 11 and matches the shape of the upper face 42, the lateral internal face 44 and the lower face 45 of the second locking piece 23.
• the second reinforcing wing 36 is fixed to the second locking piece 34 by any suitable means, for example by screwing the tab 57 of the second reinforcing wing 36 onto the lower face 45 of the second locking piece 34.
• the corner angle 37 is in the form of a metal plate bent at the angle formed by the first vessel wall 6 and the second vessel wall 7, for example 135 °.
• the corner angle 37 develops along the edge 8.
• a first section 58 of the angle bracket 37 develops in the plane of the sealing membrane 3 of the first tank wall 6.
• a second section 59 of the corner angle 37 develops in the plane of the sealing membrane 3 of the second tank wall 7.
• the end metal plate 5 of the first tank wall 6 is sealingly welded to the first section 58 of the angle bracket 37 and the metal plate 5 end of the second vessel wall 7 is sealingly welded to the second section 59 of the corner angle.
• the fixing between the corner angle 37 and the reinforcing wings 35, 36 does not need to be sealed, the sealing being provided by the corner angle 37 and the metal plates 5 of ends.
• corner angle 37 can be sealingly attached to the reinforcing wings 35, 36.
• the sealing membrane 3 of the tank walls 6, 7 can then be sealed to the wings. reinforcement 35, 36 directly.
• Such a variant is for example visible in FIG.
• the first section 58 of the angle bracket 37 is fixed to the membrane section 46 of the first reinforcing wing 35.
• the membrane section 46 of the first reinforcing wing 35 is located between the upper face 38 of the first piece 33 and a lower face 60 of the first section 58 of the corner angle 37.
• the second section 59 of the angle bracket 37 is fixed to the membrane section 54 of the second reinforcing wing 36, the membrane section 54 of the second reinforcing wing 36 is located between the upper face 42 of the second piece 34 and a lower face 61 of the second section 59 of the corner angle 37.
• the fixing of the corner angle 37 on the membrane sections 46, 54 of the reinforcing wings 35, 36 is carried out by any means adapted, for example by welding.
• the reinforcing wings 35, 36 and the corner angle 37 are made of metal sheet with a low coefficient of expansion, for example nickel alloy known as INVAR ®.
• the manufacture of the corner angle 37 is extremely simple since it is sufficient to fold a metal sheet at the desired angle, for example the angle 135 ° formed by the first tank wall 6 and the second tank wall 7 Likewise, the reinforcing wings 35, 36 are very simple to manufacture since they also require only a simple folding of metal sheet at the desired angles.
• a first sheet bending allows the formation of a 90 ° angle between the joining section 49, 56 and the tab 50, 57.
• a second folding allows the formation of an angle corresponding to the angle formed between the bisecting plane 11 and the upper face 28, 29 of the heat-insulating elements 9, 10 between the membrane section 46, 54 and the anchoring section 47, 55.
• the blocking pieces 33, 34 are also simple to manufacture since they are only wooden beams whose upper face 38, 42 is beveled according to the angle formed by the bisecting plane 11 and the face upper 28, 29 of the heat-insulating elements 9, 10.
• the anchoring piece 32 is anchored in the groove 30.
• the lateral external faces 39, 43 of the blocking pieces 33, 34 are glued respectively against the lateral internal faces 26, 27 of the half-grooves 22, 23.
• a lower face of the piece angle 32 is fixed against the bottom 31 of the groove 30.
• the end faces 12, 13 of the heat-insulating blocks of angles 9, 10 can be glued together. Such bonding between the end faces 12, 13 of the heat-insulating blocks with angles 9, 10 can be carried out continuously or discontinuously.
• traction is exerted by the sealing membrane 3 on the corner angle 37 by fixing the end metal plates 5 on the corner angle 37.
• the reinforcing wings 35, 36 being anchored to the locking pieces 33, 34, the traction is transmitted to the locking pieces 33, 34.
• the anchoring of the locking pieces 33, 34 in the groove 30 makes it possible to absorb tensile stresses.
• the realization of the corner angle 37 in the form of a continuous mechanical sheet part and the fixing of the end metal plates 5 on the corner angle 37 ensures the sealing of the sealing membrane 3 at the of the ridge 8.
• FIG. 2 is an exploded schematic perspective view of a corner piece of FIG. 1.
• the first blocking piece 33 has a countersink 63 located on a central portion of the lower face 41 of the first locking piece 33.
• the ends of the lower face 41 located on each side of the counterbore 63 form a lower end surface 65 of the first locking piece 33.
• the countersink 63 is made to a thickness substantially equal to the thickness of the lug 50 of the first reinforcing wing 34.
• a plurality of screw holes are located regularly in a bottom of the counters 63.
• the first locking piece 33 has, on its lateral external face 39 at the ends of the lower end surfaces 65, nut housings 66 of complementary shapes to the nuts 67.
• a bottom nut housing 66 has a hole through (not shown). This through hole opens on the one hand on the lateral internal face 40 of the first locking piece 33 and, on the other hand, on the bottom 68 of said nut housing 66.
• This through orifice has a diameter slightly greater than the portion threaded 64 of a clamping screw 70.
• the second locking piece 34 has on its underside 45 a counterbore 71 and lower end surfaces 72 similar to the counterbore 63 and the end surfaces 65 described above opposite the first locking piece 33.
• the second locking piece 34 has on its lateral internal face 44, vis-à-vis each through-hole of the nut housings 66 of the first locking piece 33, through openings 73.
• a through hole 73 of the second piece of blocking 34 opens on the one hand on the lateral internal face 44 of the second locking piece 34 and, secondly, in a clamping screw head housing.
• This through orifice 73 has a diameter slightly greater than the diameter of the threaded portion 64 of the clamping screw 70.
• a screw head housing (not shown) is located on the lateral external face 43 of the second locking piece 34 at the right of each lower end surface 72 and is of complementary shape to a head 75 of the clamping screw 70. .
• the reinforcing wings 35, 36 are developed only at the counterbores 63, 71 of the blocking pieces 33, 34.
• the length along the axis of the edge 8 of the reinforcing wing 35, 36 is equal to the length of the counterbores 63, 71 along the same axis of the edge 8.
• the length along the axis of the edge 8 of the corner angle 37 is equal to the length of the counterbores 63, 71 along the same axis of the edge 8.
• the anchoring sections 47, 55 and the membrane sections 46, 54 of each reinforcing wing 35, 36 are developed only between two planes perpendicular to the axis of the 8 and contiguous edges of both counters 63, 71 and lower end surfaces 65, 72.
• the corner angle 37 is also developed only between these two planes perpendicular to the axis of the edge 8 and joined to both counterbores 63, 71 and lower end surfaces 65, 72.
• Figure 3 shows a schematic perspective view of a corner piece of Figure 1 mounted.
• the tabs 50, 57 of the reinforcement wings 35, 36 are housed in the counterbores 63, 71 of the lower faces 41, 45 of the locking pieces 33, 34.
• a lower face 76, 77 lugs 50, 57 is flush with liveau end lower surfaces 65, 72.
• the legs 50, 57 ⁇ enfort wings 35, 36 are screwed to blockages parts 33, 34 by a plurality of screws 8 screwed into the locking pieces 33, 34 at the countersinks 63, 71.
• the first locking piece 33 is connected to the second locking piece 34 by the clamping screws 70.
• the head 75 of the clamping screws 70 bears against the bottom of the screw head housings of the second locking piece 34.
• the nuts 67 are mounted on the threaded portion 64 of the screw 70 and bear against the bottom 68 of the nut housings 66 of the first locking piece 33.
• corner pieces 32 extend into the groove 30 substantially all along the longitudinal edge 8.
• a plurality of corner pieces 32 are anchored to each other. following the others in the groove 30.
• the corner piece 32 is anchored by gluing in the groove 30 both at the lower end surfaces 65, 72 of the locking pieces 33, 34 and lower faces 76, 77 tabs 50, 57 of the reinforcing wings 35, 36.
• Such a weld strip also covers the upper face of the ends of two locking pieces 33, 34 consecutive not covered by the reinforcing wings 35, 36. This welding strip seals the sealing membrane 3 between two pieces 32 consecutive angles along an edge 8.
• Figure 4 shows a schematic perspective view of an embodiment of the corner piece 32 in the mounted state.
• the locking pieces and the reinforcing wings have the same characteristics as the locking pieces and the reinforcing wings of Figure 2 and have the same references.
• the blocking pieces 33, 34 are interconnected by the clamping screws 70 and the nuts 66 as described with reference to FIGS. 2 and 3.
• the corner angle 37 has a shape similar to that of the corner pieces of Figures 2 and 3 but has different dimensions along the axis of the edge 8.
• a first longitudinal end 98 of the corner angle 37 extends outwardly of the corner piece 32 beyond the blocking pieces 33, 34 along the axis of the edge 8.
• a second longitudinal end 99 of corner angle 37, opposite the first longitudinal end 98, develops, projection in a plane parallel to the axis of the edge 8, between the membrane sections 46, 54 of the reinforcing wings 35, 36 and an extreme longitudinal face 100 of the corner piece 32.
• the corner pieces 32 are mounted in the groove 30 juxtaposed to each other along the longitudinal edge 8 all along said 8.
• a first corner piece is mounted in the groove 30 so that the first longitudinal end 98 of its corner angle 37 covers the second longitudinal end 98 of a second adjacent corner piece.
• the first longitudinal end 98 of the corner angle 37 of the first corner piece is then sealingly attached to the second longitudinal end 98 of the corner angle 37 of the second corner piece.
• corner pieces 32 according to this embodiment do not require the installation of a weld strip as is the case for corner pieces of Figures 2 and 3. A single sealed weld is required and sufficient to ensure tightness between two consecutive corner pieces in the groove.
• FIG. 5 represents a sectional view of a vane angle as in FIG. 1 at the level of a mechanical element linking the first locking piece and the second locking piece in which the connection between the first locking piece 33 and the second locking piece 34 is made elastically.
• a connection can be made by any suitable means, for example by inserting Belleville washers 80 between the nut 67 and the bottom 68 of the nut housing 66. These Belleville washers 80 allow a flexibility in the mechanical connection between the pieces of blocking 33 and 34. In this variant, the heat-insulating elements of angles 9, 10 of the cell walls 6, 7 are not glued together.
• the double-diaphragm tank comprises, from the bearing structure to the inside of the tank, a secondary insulating barrier 2A, a secondary sealing membrane 3A, a primary insulating barrier 2B and a primary sealing membrane 3B .
• the secondary sealing membrane 3A forms a secondary edge 8A and the primary sealing membrane 3B forms a primary edge 8B.
• the secondary insulating barrier 2A comprises heat-insulating elements of angle 9A, 10A as described above and the primary insulating barrier 2B has heat-insulating elements of angle 9B, 10B as described above.
• a secondary corner piece 32A as described above is anchored in a secondary groove 30A formed by the secondary corner heat-insulating elements 9A, 10A of the secondary insulating barrier 2A.
• a primary corner piece 32B is anchored in a primary groove 30B formed by the primary corner heat insulating elements 9B, 10B of the primary insulating barrier 2B.
• Secondary metal end plates 5A of the first vessel wall 6 are sealingly anchored to the secondary corner piece 32A.
• the secondary metal plates 5A of the second vessel wall 7 are sealingly anchored to the secondary corner piece 32A.
• the primary metal plates 5B of the first tank wall 6 are sealingly anchored to the primary corner piece 32B.
• the primary metal plates 5B of the second vessel wall 7 are sealingly anchored to the primary corner piece 32B.
• An end face 12A, 13A of the heat-insulating elements 9A, 10A of the secondary insulating barrier 2A located in the bisecting plane 11 are glued sets.
• An end face 12B, 13B of the heat-insulating elements 9B, 10B of the primary insulating barrier 2B located in the bisecting plane 11 are glued together.
• FIG. 7 shows a cut-away view of the vial angle of FIG. 6 in which the corner piece is modified: stiffeners 81 are installed between the lug 57B and the junction section 56B of the anchoring section 55B of the second primary reinforcement wing 36B.
• Stringers 81 B are spaced evenly along the second end 62B of the connecting section 56B of the second primary reinforcing wing 36B. These stiffeners 81 B are for example simple pieces of flat triangular metal sheets developing in planes perpendicular to the direction of the edge 8.
• the second secondary blocking part 34B advantageously comprises grooves (not shown) of complementary shapes of the stiffeners B. The stiffeners 81 B are housed in these grooves.
• the tab 57B is pulled toward the joining section 56B of the second primary reinforcing wing 36B and, in the manner of a paper sheet conforming to the contours of a projecting right angle, the fold between the connecting section 56B and the tab 57B tends to move along the anchor section 55B and decrease the width of the tab 57B along an axis perpendicular to the bisecting plane 11.
• stiffeners 81 B In the presence of such stiffeners 81 B, the screw fixing between the tab 57B and the second secondary locking piece 34B can even be removed, the conservation characteristics of the fold between the connecting section 56B and the tab 57B associated with the complementarity of the anchoring section 55B with the second locking piece 34 makes it possible to maintain the second reinforcing wing 36 against the second locking piece 34 even in presence of constraints.
• Such stiffeners 81 B can also be installed on each reinforcing wing 35, 36 of each sealing membrane 3A, 3B.
• a secondary metal intermediate plate is sealingly fastened to the secondary corner angle 37A, the end metal plates (not shown) of the tank walls 6, 7 being sealingly attached to this intermediate metal plate.
• Figure 8 shows a cutaway view of the sealed and thermally insulating vessel angle with the double sealing membrane and the double insulating barrier. At the edge, the primary insulating barrier and the primary waterproofing membrane are omitted to show the corner piece provided at the secondary sealing membrane.
• the secondary sealing membrane 3A comprises a plurality of side corrugated metal sealing plates 5A juxtaposed. These secondary corrugated metal plates 5A are fixed sealingly to each other.
• the secondary insulating barrier 2A comprises a plurality of secondary heat insulating elements 4A.
• An upper face of the secondary heat-insulating elements 4A comprises metal anchoring blades 82A on which are anchored the corrugated metal plates 5A of the secondary sealing membrane 3A.
• a protective shell 83 covers the corrugations of the secondary metal sealing plates 5A.
• Primary heat-insulating elements 4B rest on the protective shell 83.
• An upper face of the primary heat-insulating elements 4B includes anchor blades 82B on which are anchored the primary corrugated sealing plates 5B. These primary corrugated sealing plates 5B are intended to be in contact with LNG stored in the tank 1.
• a plurality of secondary angle heat insulating elements 9A, 10A are located along the secondary edge 8A.
• the secondary angle heat insulating elements 9A, 10A form the secondary groove 30A extending along the secondary edge 8A.
• Each secondary corner heat-insulating element 9A, 10A has a countersink on its upper face 28A, 29A.
• a plurality of metal blades 84 are accommodated in the countersinks of the upper faces 28A, 29A of secondary angle heat insulating elements 9A, 10A.
• a plurality of secondary corner pieces 32A are anchored one after the other in the secondary groove 30A.
• the membrane sections 46A, 54A of the secondary reinforcing wings 35A, 36A of each anchor piece 32A are fixed to the metal plates 84 of the heat-insulating elements 9A, 10A. This fixing is carried out by any suitable means, for example by welding.
• the membrane sections 46A, 54A of the secondary reinforcing wings 35A, 36A have a second end 85 opposite the first end 48A of the membrane sections 46A, 54A of the reinforcing wings 35A, 36A.
• the secondary metal end plates 5A of the first vessel wall 6 are sealingly anchored to the second end 85 of the first secondary reinforcing wing 35A opposite the first end 48A of the membrane section 46A.
• the first secondary corner angle section section 37A 37A is sealingly welded to the membrane section 46A of the first secondary reinforcement wing 35A.
• the secondary metal end plates 5A of the second vessel wall 7 are sealingly anchored on the end 85 of the membrane section 54 of the second secondary reinforcing wing 36B.
• the second section 59A of the secondary corner angle 37A is sealingly attached to the membrane section 54A of the second secondary reinforcing wing 36B.
• a secondary weld strip is sealingly attached to the ends of two consecutive secondary anchoring pieces 32A in the direction of the secondary edge 8A so as to seal the secondary sealing membrane 3A at the level of the secondary edge 8A.
• the primary corner heat insulating elements 9B, 10B and the corner pieces (not shown in FIG. 8) have a similar configuration to the secondary corner heat insulating elements 9A, 10A and the secondary corner pieces 32A.
• the sealing membranes can be made in different ways on the flat walls.
• the primary waterproofing membrane comprises a plurality of corrugated plates as in FIG. 8 and the secondary waterproofing membrane consists of a plane waterproof layer produced for example by a sheet of waterproof composite material bonded to the secondary insulating barrier as described in FR2691520.
• Figure 9 is a schematic perspective cutaway view of an alternative embodiment of a vane angle of Figure 8 having a plurality of corner angles according to another embodiment.
• the secondary sealing membrane 3A comprises a plurality of side corrugated metal sealing plates 5A juxtaposed. These secondary corrugated metal plates 5A are fixed sealingly to each other. Similarly, a plurality of primary corrugated sealing plates 5B intended to be in contact with LNG stored in the tank 1 are sealed to each other to form the primary sealing membrane 3A.
• a plurality of primary angle heat insulating elements 9B, 10B are located along the primary edge 8B. These primary corner heat insulating elements 9B, 10B are based on a secondary protective shell covering the secondary corner pieces 32A.
• a plurality of primary corner pieces 32B are anchored one after the other in the primary groove (not shown).
• the primary corner angles cover the membrane sections 46B, 54B of the primary reinforcing wings 35B, 36B of each primary anchoring piece 32B.
• the primary metal end plates 5B of the first vessel wall 6 are sealingly anchored to the first section 58B of the primary angle bracket 37B and the primary metal end plate 5B of the second vessel wall 7 is sealingly welded to the second section 59B of the primary corner angle 59B.
• the primary corner pieces 32B consecutive along the primary edge 8B overlap as described with reference to Figure 4.
• a sealed seal is formed on the ends of two consecutive primary corner pieces 32B in the direction of the primary edge 8B so as to seal the primary waterproofing membrane 3B at the primary edge 8B.
• each corner angle 37A, 37B has a 101A wave 101B stamped.
• These waves 101A, 101B are for example centrally located on each corner angle 37A, 37B, halfway between the two opposite ends along the axis of the edge 8 of said angle brackets 37A, 37B.
• These waves 101A, 101B develop from the end of the first section 58A, 58B corner angles 37A, 37B on which are fixed the end metal plates 5A, 5B of the first tank wall 6 up to at the end of the second section 59A, 59B of said corner angles on which are fixed the metal end plates 5A, 5B of the second vessel wall 7.
• waves 101A, 101B are advantageously developed in each section 58A, 58B, 59A, 59B angle brackets 37A, 37B perpendicular to the axis of the edge 8.
• the waves 101A, 101B develop towards the inside of the tank.
• the secondary protective shell on which the primary heat-insulating elements rest preferably covers the waves 101A of the secondary corner angles 37A.
• Such corner pieces in addition to allowing the anchoring of the membranes on the heat-insulating elements of angle, offer a continuous flexibility along the edge 8 by allowing the stresses to be absorbed by deformation of the waves 101A, 101B
• the angle is made in INVAR®, the height of these waves is reduced compared to the height of the waves 101A, 101 B located on the corrugated metal plates, the weak contraction of the INVAR® allowing only a limited deformation corner pieces 32.
• the secondary membrane and / or the primary membrane consist of a plurality of straightened strakes. sealed to each other by means of welding supports, as described in FR2709725. Other metal membranes can still be used.
• FIGS 11 to 15 show an embodiment wherein the planar walls of the vessel are formed from prefabricated parallelepiped blocks similar to those described in FR2691520. Elements similar or identical to those of Figures 1 to 9 have the same reference numeral increased by 200.
• the vessel has a double membrane.
• the secondary insulating barrier, the secondary waterproof membrane and the primary insulating barrier of the tank are essentially formed by assembling a plurality of prefabricated blocks juxtaposed on the supporting structure.
• Planar prefabricated blocks 102 are juxtaposed to form the flat walls of the tank and prefabricated corner blocks 103 are arranged at the corners of the tank.
• Each prefabricated plane block 102 comprises, from the supporting structure 1 towards the inside of the vessel:
• a bottom panel 104 of rectangular shape for example of plywood
• a block of rectangular insulating foam 105B rectangular rectangle of smaller dimensions and disposed co-axialemerit to the block of secondary insulating foam 105A so that the block of primary insulating foam 105B covers only partially the waterproof film 106 and leaves visible a strip of waterproof film 106 on the periphery of the prefabricated block plane 102, and
• cover panel 107 for example made of plywood covering the block of primary insulating foam 105B.
• the sealed film layer 106 in the prefabricated planar blocks is for example formed by a multilayer composite material comprising a thin sheet of metal sandwiched between two fiberglass fabrics that are stuck together.
• a waterproof film is known as TRIPLEX®.
• a prefabricated corner block 103 intended to be installed at an angle of the tank formed by the first wall 6 and the second tank wall 7 comprises:
• the locking pieces 233, 234 are wider, in a direction perpendicular to the edge 8 and parallel to the tank wall that they are thick, in a direction perpendicular to the tank wall.
• the upper face of the locking pieces 233, 234 comprises a countersink 1 12.
• This countersink 1 12 is intended to receive the membrane section 246, 254 of the reinforcing wings 235, 236.
• the membrane sections 246, 254 of the reinforcement wings 235, 236 are narrower than the locking pieces 233, 234 so that the diaphragm sections 246, 254 rest integrally on the locking pieces 233, 234.
• a first screw 270 is disposed at the end of the locking pieces 233 and 234 beyond the reinforcing wings 235 and 236. in a similar manner to Figure 2.
• the nut housing as described with reference to Figure 2 is located on the lower face 241 of the first blocking part 233.
• the housing. screw head (not shown in Figure 1 1) is located on the underside 245 of the second locking piece 234.
• the nut housing 266 and the screw head housing 115 open on the lower faces 241, 245 of the locking pieces 233, 234 to the right of the reinforcing wings 235 and 236.
• the joining sections 249, 256 of the reinforcing wings 235, 236 have orifices 116 allowing the passage of the screw 114.
• the first impervious film 110 is of the same nature as the impervious film 106 used in the prefabricated planar blocks 102.
• the second impervious film 11 covers only partially the block of secondary insulating foam 109.
• the first impervious film 110 is thus visible on any a peripheral surface of the prefabricated corner biocoil 103.
• the blocking pieces 233, 234 only partially cover the second impervious film 111 so that a peripheral band of the second impervious film 11 is visible all around the blocking pieces 233, 234.
• the locking pieces 233, 234 are glued directly onto the second waterproof film 111.
• FIG. 12 is a partial diagrammatic perspective view of an assembly of two prefabricated corner blocks of FIG. 11.
• Fig. 12 As in Fig. 11, the primary waterproofing membrane is not shown.
• the juxtaposition of two prefabricated corner blocks 103 forms a joint space 17.
• the illustration in Figure 12 of this joint space 117 is amplified for a better understanding of the assembly only. In practice, the space 117 is reduced to the minimum possible and is filled by an insulator during assembly of the tank, for example glass wool.
• a flexible waterproof film strip 118 covers the space 1 17 in order to seal the secondary waterproofing membrane to the right of this space 117.
• the waterproof film strip 118 is bonded to the two prefabricated corner blocks 103 juxtaposed on either side of the space 117 and extends to the second tight film 111 of each prefabricated block angle 103.
• an insulating junction block 119 covers the waterproof film strip 118.
• Each insulating block of junction 119 is generally L-shaped with a first layer of primary insulating foam covered by a first cover panel and a second layer of primary insulating foam covered by a second cover panel.
• the first layer of primary insulating foam and the first cover panel of the joint insulating block 119 each develop parallel to the first vessel wall.
• the second primary insulating foam layer and the second cover panel of the joint insulating block 119 each develop parallel to the second vessel wall.
• An upper face of each cover panel of the insulating junction block 119 has fastening plates 120.
• the insulating junction block 1 19 grows along the edge 208 in contiguous manner with the blocking pieces 233, 234 of the two corner prefabricated blocks 103 juxtaposed.
• the first cover panel of the insulating junction block 1 9 is flush with the upper surface of the first blocking piece 233.
• the second cover panel of the junction isolating block 119 is flush with the top surface of the second piece of block. 234.
• external lateral faces of the insulating junction blocks 119 are flush with the external lateral faces 239, 243 of the blocking pieces 233, 234.
• the prefabricated corner blocks 103 illustrated in FIG. 12 may be installed in a polygonal cylinder shaped earth tank.
• a land tank has a plurality of vertical walls arranged to form a polygonal cylinder.
• the two prefabricated corner blocks 103 of FIG. 12 have a slight angle at the space 117 which corresponds to the angle between two successive sides of the polygon.
• the general form of such a vessel is for example described in the document FR2951521.
• FIG. 13 represents an enlarged partial view of the zone XIII of FIG. 12 which makes visible a lower angle plate 121 fixed on the reinforcing wings 235 and 236.
• the angle iron will finally be made in two parts.
• the lower corner plate 121 is welded together on the membrane sections 246, 254 of the reinforcing wings 235, 236.
• An upper corner plate 122 (see FIGS. ), for example in INVAR® will then be welded together on the lower corner plate 121 and on the fixing plates 120.
• the prefabricated planar blocks 102 are juxtaposed to form the flat walls of the tank and the prefabricated blocks of angle 103 are arranged along the edge 208 at the junction of two flat walls.
• secondary sealing film strips 123 and primary insulating tiles 124 are installed between all adjacent prefabricated blocks, similarly to the as described in document FR2691520.
• the secondary sealing film strips 123 are sealingly bonded to the sealed films 106, 110 of the adjacent prefabricated blocks.
• the primary insulating blocks 124 cover the edge of the adjacent prefabricated blocks 102 and 103.
• the primary insulating barrier thus comprises an insulating foam layer formed by the primary insulating foam blocks of the prefabricated planar blocks 102, the primary insulating blocks 124 and the insulating junction blocks 119.
• this layer of insulating foam present at the prefabricated corner blocks 103 a groove 230 in which are housed the corner piece 232 formed by the locking pieces 233, 234 and the reinforcing wings 235, 236.
• the groove 230 extends over the entire thickness of the primary insulating barrier.
• the bottom 231 of the groove 230 is formed in this embodiment by the sealed films 1 10 and 111 of the prefabricated corner block 103.
• the inner side faces of each half-groove are formed by the sides of the primary insulating tiles. 124 jointly covering the prefabricated corner block 103 and the prefabricated plane block 102.
• Fig. 14 further shows an upper corner plate 122 arranged along the edge 208 on the lower corner plates 121. Furthermore, the primary membrane is omitted in Fig. 14.
• the upper corner plates 122 illustrated in FIG. 14 comprise on the edge of their first and second sections 258, 259 intended to be covered by the sealing membranes of the tank walls, fixing holes 125 intended to receive screws. with wood (not shown) screwed into the plywood cover panels of the insulating blocks 124.
• These fixing holes 125 are preferably oblong in a direction perpendicular to the edge 208 to preserve a small sliding clearance of the corner plate upper 122 relative to the insulating pad 124.
• the upper corner plates 122 also have oblong attachment holes 126 located at the lower corner plate 121.
• the upper corner plates 122 are welded at the edge of the oblong mounting holes 126 on the plates. lower angle 121 in order firstly to seal the primary waterproofing membrane and, secondly, the anchoring of the upper corner plates 122 on the lower corner plates 121.
• the upper corner plates 122 have circular orifices 127 for anchoring the upper corner plates 122 on the fastening plates 120 of the junction insulating blocks 119.
• the upper corner plates 122 have at the junction insulating blocks 119 arranged between two prefabricated corner blocks 103 a groove 128, shown in dotted lines in FIG. 14, on the walls.
• This groove 128 provides sufficient flexibility to the upper corner plate 122 to develop jointly on the two prefabricated corner blocks 103 juxtaposed despite the presence of an angle between said two prefabricated corner blocks 103.
• a waterproof strip 129 seals the primary waterproofing membrane at this groove 128.
• the upper angle plates may comprise a corrugation 130 developing towards the interior of the vessel in order to absorb the stresses at the angles of the vessel.
• the lower corner plate is omitted and the upper corner plate 122 is directly welded to the reinforcing wings 235, 236.
• the technique described above for producing a sealed and thermally insulating tank can be used in different types of tanks, for example for example, to constitute a sealed and thermally insulating tank of an LNG tank in a terrestrial installation or in a floating structure such as a LNG tanker, or to constitute a smaller volume, sealed and thermally insulating tank to serve as a feed tank for a propulsion machine.
• a tank has a volume of between 5000 and 30,000 m 3 .
• a cutaway view of a LNG carrier 86 shows a sealed and insulated tank 87 of prismatic general shape mounted in the double hull 88 of the ship.
• the wall of the tank 87 comprises a primary sealed barrier intended to be in contact with the LNG contained in the tank, a secondary sealed barrier arranged between the primary waterproof barrier and the double hull 8 of the vessel, and two insulating barriers arranged respectively between the primary watertight barrier and the secondary watertight barrier and between the secondary watertight barrier and the double hull 88.
• loading / unloading lines 89 arranged on the upper deck of the ship can be connected, by means of appropriate connectors, to a marine or port terminal to transfer a cargo of LNG from or to the tank 87.
• FIG. 10 represents an example of a marine terminal comprising a loading and unloading station 90, an underwater pipe 91 and an onshore installation 92.
• the loading and unloading station 90 is a fixed off-shore installation comprising an arm mobile 93 and a tower 94 which supports the movable arm 93.
• the movable arm 93 carries a bundle of insulated flexible pipes 95 that can connect to the loading / unloading pipes 89.
• the movable arm 93 can be adapted to all gauges of LNG carriers .
• a link pipe (not shown) extends inside the tower 94.
• the loading and unloading station 90 enables the loading and unloading of the LNG carrier 86 from or to the shore facility 92.
• the subsea pipe 91 allows the transfer of the liquefied gas between the loading or unloading station 90 and the onshore installation 92 over a large distance, for example 5 km, which keeps the LNG vessel 86 at a great distance from the coast during the loading and unloading operations.
• pumps on board the ship 86 and / or pumps equipping the shore installation 92 and / or pumps equipping the loading and unloading station 90 are used.
• corner pieces as described above can also be placed along any edge of a tank, for example an edge of a tank forming a 90 ° angle or any other angle.
• first blocking piece 33 and / or the second blocking piece 34 may be made of any material other than the suitable wood, for example high density foam of the order of 210 kg / m 3 or more by example.
• high density foam of the order of 210 kg / m 3 or more by example.
• the use of such a high-density foam for the production of the blocking pieces 33, 34 makes it possible to have homogeneity in the bonding of the blocking pieces 33, 34 in the half-grooves 22, 23.
• the use of high density foam decreases the thermal contraction differential between the heat-insulating elements of angle 9, 10 and the locking pieces 33, 34.
• the blocking pieces 33, 34 may have a lower face 41, 45 larger than their lateral external face. , 43.

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• 2013
  • 2013-08-15 FR FR1358031A patent/FR3009745B1/fr active Active
• 2014
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